Boeing 727-25C

Service difficulty reports · 2,007

Newest first. General aviation reporting is voluntary.

Query with SQL
duckdb -csv -c "SELECT sdr_id, difficulty_date, n_number, aircraft_make, aircraft_model, part_name, part_condition, jasc_code, discrepancy
  FROM 'https://openairdocs.org/data/latest/faa_service_difficulty_report.parquet'
  WHERE aircraft_model_key = '72725C'
  ORDER BY difficulty_date DESC"

Prints the whole list as CSV. It reads the release’s Parquet files over HTTPS, so there’s nothing to download first. Install DuckDB to run it.

SDR UPS96220181Stringer Tie · crackedINSPECTION TYPE: C. STA 9700 AT STR 4L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220180Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 5L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220179Stringer Tie · crackedINSPECTION TYPE: C. STA 970 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220178Stringer Tie · crackedINSPECTION TYPE: C. STA 990 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220177Stringer Tie · crackedINSPECTION TYPE: C. STA 990 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220176Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220175Stringer Tie · crackedINSPECTION TYPE: C. STA 1030 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220174Stringer Tie · crackedINSPECTION TYPE: C. STA 1030 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220173Stringer Tie · crackedINSPECTION TYPE: C. STA 1030 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220172Stringer Tie · crackedINSPECTION TYPE: C. STA 1050 AT STR 4L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220171Stringer Tie · crackedINSPECTION TYPE: C. STA 1050 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220170Stringer Tie · crackedINSPECTION TYPE: C. STA 1070 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220169Stringer Tie · crackedINSPECTION TYPE: C. STA 1030 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220168Stringer Tie · crackedINSPECTION TYPE: C. STA 1050 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220167Stringer Tie · crackedINSPECTION TYPE: C. STA 1070 AT STR 6L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220166Stringer Tie · crackedINSPECTION TYPE: C. STA 1070 AT STR 9L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220165Stringer Tie · crackedINSPECTION TYPE: C. STA 1090 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220164Stringer Tie · crackedINSPECTION TYPE: C. STA 1030 AT STR 3R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220163Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 7L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220162Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 8L, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE. FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220161Stringer Tie · crackedINSPECTION TYPE: C. STA 1090 AT STR 5R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220160Stringer Tie · crackedINSPECTION TYPE: C. STA 1050 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220159Stringer Tie · crackedINSPECTION TYPE: C. STA 1030 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220158Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 7R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220157Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 4R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220156Stringer Tie · crackedINSPECTION TYPE: C. STA 990 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220155Stringer Tie · crackedINSPECTION TYPE: C. STA 990 AT STR 4R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220154Stringer Tie · crackedINSPECTION TYPE: C. STA 970 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220153Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 6R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-2, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220152Stringer Tie · crackedINSPECTION TYPE: C. STA 1010 AT STR 9R, STRINGER TIE IS CRACKED. REMOVED STRINGER TIE, FABRICATED REPLACEMENT PART AND INSTALLED PER SRM 51-10-1, SRM 51-30-1, AND SRM 53-10-2.May 8, 1996 · N946UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220584Frame · corrodedINSPECTION TYPE-C, RIGHT SIDE FRAME 760, FWD EDGE OF RT FWD EMERGENCY EXIT HAS TWO SMALL AREAS OF INTERGRANULAR CORROSION ON INNER FLANGE STRAP AT STRINGERS 16R AND 17R. REMOVED FASTENERS AND CORROSION PER SRM 51-30-2 AND 51-10-6, BLENDED AREA AND FINISHED PEMay 7, 1996 · N946UP · Boeing 72725C · Fuselage Main, FrameSDR UPS96220068Stiffener · corrodedINSPECTION TYPE 'C', CORROSION ON LT WING FRONT SPAR VERT STIFFENER 5TH STIFFENER O/B FROM ACCESS CUTOUT 7340. REMOVED CORRODED STIFFENER, INSTALLED NEW SIFFENER PER SRM 51-3-2, 57-10-4 AND MM 28-11-0.May 7, 1996 · N937UP · Boeing 72725C · Wing Miscellaneous StructureSDR 96FDEA00904Retract Mech · malfunctionedAFTER LANDING RETRACTION, LANDING HANDLE PLACED TO OFF, RED DOORS LIGHT ILLUMINATED ALONG WITH RT MAIN GEAR DOOR LT ON S/O PANEL. VIBRATION WAS FELT. PERFORMED ABNORMAL LIST AND PROCEEDED WITH LEVER IN UP POSITION. INSTALLED GEAR PINS - INSP RT GEAR DOOR -May 7, 1996 · N127FE · Boeing 72725C · Landing Gear Retraction/Extension SystemSDR UPS96220067Nose · corrodedINSPECTION TYPE 'C' AILERON SERVO HOUSING IN FWD NOSE COMP IS CORRODED. REMOVED CORRODED HOUSING, INSTALLED NEW HOUSING PER MM 22-11-11.May 6, 1996 · N937UP · Boeing 72725C · AileronsSDR UPS96220066Fitting · corrodedINSPECTION TYPE 'C', CENTER HINGE 0N RT WING AILERON TAB AILERON SIDE IS CORRODED. REMOVED CORRODED HINGE FITTING AND INSTALLED NEW HINGE FITTING PER SRM 51-30-2 AND MM 27-10-11.May 6, 1996 · N937UP · Boeing 72725C · Aileron TabsSDR 96FDEA00915Gusset · crackedCABIN INTERIOR STA FS 600 RIB GUSSET IS CRACKED IN TWO AT STR 2L AREA. REPLACED GUSSET WITH 7075-T6 X.063 DOUBLER AS SHOWN IN FIG NR 1 AS PER EA 7-5330-28637 DATED APRIL 30 1996.May 6, 1996 · N124FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220064Door Gate · crackedINSPECTION TYPE 'C', MID GALLEY DOOR UPPER GATE BEAM CRACKED ON I/B RADIUS ALL AFT SIDE. REMOVED AND REPLACED BEAM IAW SRM 51-30-2, 51-20-4 AND MM 52-12-11.May 3, 1996 · N937UP · Boeing 72725C · Galley DoorsSDR 96FDEA00912Web · crackedLT STA 870 LOWER INTEGRAL WEB IS CRACKED. FABRICATED A MACHINED BATHTUB FITTING. MATERIAL TO BE 4130 TREATED TO SPECIFICATION 180 TO 200 KSI CAD PLATE, PRIME AS REQUIRED. INSTALLED BATHTUB FITTING PER ESO 11782 DATED 04-22-96 AND EA 7-5310-28607. REF SHOP May 2, 1996 · N124FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR UPS96220065Intercostal · corrodedINSPECTION TYPE 'C', CORROSION ON THE INTERCOSTAL AT BS 1045, RBL 6 WL 146. REMOVED CORROSION AND REPAIRED INTERCOSTAL IAW SRM 51-30-2, 51-10-2 AND MM 51-20-15.May 1, 1996 · N937UP · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01047Door Frame · crackedCRACK IN LWR FWD CORNER OF DOOR FRAME OF FWD LWR CARGO APPROX 1 INCH LONG. STOP DRILLED CRACK AND INSTALLED 7075-6, 0.90 DOUBLER ANGLE PER SRM 53-10-4 PG 39 TO 41.Apr 30, 1996 · N136FE · Boeing 72725C · Fuselage Miscellaneous StructureSDR 96FDEA01046Stringer · corrosionCORROSION STA 6L STA 848 TO 870 UPPER LOBE. CUT CORROSION OUT, INSTALLED STR DOUBLER PER SRM 53-10-3 PG 5 TO 8.Apr 30, 1996 · N120FE · Boeing 72725C · Fuselage Main, Longeron/StringerSDR CA970305001Combustion Case · liberated(CAN) THE ENGINE WAS REMOVED AND SENT FOR INVESTIGATION DUE TO HIGH EGT AND TREND ANALYSIS THAT INDICATED HOT SECTION DISTRESS. INVESTIGATION FOUND THE INNER COMBUSTION CASE HAD LIBERATED FROM THE FORWARD FLANGE. IT APPEARED TO SUFFER FROM METAL FATIGUE. ALL TApr 29, 1996 · Boeing 72725C · Turbine Engine Combustion SectionSDR 96FDEA01045Spar · crackedLT WING FRONT SPAR UPPER CHORD CRACKED ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. REMOVED CRACK, VOID IN CORROSION AND CORROSION ABOVE AND O/B OF NR 2 LE FLAP ACTUATOR. INSTALLED REPAIR DOUBLER PER FEDEX EA 7-5710-28691 DATE 5-22-96.Apr 29, 1996 · N120FE · Boeing 72725C · Wing SparSDR UPS96205991Escape Rope Door · out of adjustMAINTENANCE REPORTED, ESCAPE ROPE DOOR ON CAPT'S SIDE WILL NOT STAY CLOSED. TRIMMED DOOR SO AS TO NOT INTERFERE WITH LATCHING MECHANISM. CYCLED DOOR SEVERAL TIMES, DOOR OPENS, CLOSES AND LOCKS GOOD.Apr 16, 1996 · N951UP · Boeing 72725C · Emergency ExitsSDR 96FDEA00810Frame · crackedNRO232, STA 804 ABOVE CUSP, FRAME CRACKED FROM I/B LIP TO FASTENER HOLE IN CENTER OF FRAME. *S/D* FABRICATED REPAIR PARTS IAW SRM 51-40-3 AND INSTALLED DOUBLER IAW SRM 51-40-3.Apr 16, 1996 · N124FE · Boeing 72725C · Fuselage Main, FrameSDR UPS96205974Support Fitting · misdrilledWHILE IN FOR C-CHECK, MAINTENANCE REPORTED DOUBLE HOLE IN HOR FLANGE OF RT MLG SUPPORT FITTING BS 940 RBL 66 WL 208. REMOVED DAMAGED AREA AND REPAIRED PER EO 727-53-1754.Apr 12, 1996 · N933UP · Boeing 72725C · Fuselage, Landing Gear Attach FittingsSDR UPS96205973Bullnose · corrodedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED NR 1 BULLNOSE I/B LUG CORRODED. REMOVED AND REPLACED NR 1 K-FLAP BULLNOSE IAW MM 27-81-0 AND OHM 57-51-01.Apr 11, 1996 · N933UP · Boeing 72725C · Leading Edge DevicesSDR UPS96220048Forging · crackedINSPECTION TYPE C-NFEC, DET A CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT 1ST HOLE OF STA 1233 BOTTOM ROW OF FASTENERS. CRACK IS 1 INCH LONG AND RUNS A FT OF HOLE. STOP DRILLED CRACK, REPAIRED PER DRAWING 65-62346 AND SRM 51-30-2.Apr 10, 1996 · N948UP · Boeing 72725C · Vertical Stabilizer, Spar/RibSDR UPS96220047Forging · crackedINSPECTION TYPE C-HFEC INSP, DET CRACK ON RT SIDE OF VERT STAB FRONT SPAR FORGING AT FIRST HOLE AFT OF STA 1233 TOP ROW OF FASTENERS. CRACK IS .5 INCH LONG RUNS AFT OF HOLE. STOP DRILLED CRACK, REPAIRED VERT STAB CRACK PER DRAWING 65-62346 AND SRM 51-30-2.Apr 10, 1996 · N948UP · Boeing 72725C · Vertical StabilizerSDR UPS96205971Skin · delaminatedWHILE IN FOR C-CHECK, MAINTENANCE REPORTED RT AFT O/B FLAP 3 FEET I/B, 1 INCH LONG BY .125 INCH WIDE DELAMINATION MPIP-6098. REPAIRED PER SRM 51-40-06.Apr 8, 1996 · N933UP · Boeing 72725C · Trailing Edge Flaps
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